US20060225419A1 - Turbocharger - Google Patents

Turbocharger Download PDF

Info

Publication number
US20060225419A1
US20060225419A1 US11/399,775 US39977506A US2006225419A1 US 20060225419 A1 US20060225419 A1 US 20060225419A1 US 39977506 A US39977506 A US 39977506A US 2006225419 A1 US2006225419 A1 US 2006225419A1
Authority
US
United States
Prior art keywords
oil
motor
compressor
turbocharger
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
US11/399,775
Other versions
US7360361B2 (en
Inventor
Thomas Prusinski
Peter Hofbauer
Jason Schmidt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Advanced Propulsion Technologies Inc
Applied Technologies Inc
Original Assignee
Applied Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Applied Technologies Inc filed Critical Applied Technologies Inc
Priority to US11/399,775 priority Critical patent/US7360361B2/en
Publication of US20060225419A1 publication Critical patent/US20060225419A1/en
Application granted granted Critical
Publication of US7360361B2 publication Critical patent/US7360361B2/en
Assigned to ADVANCED PROPULSION TECHNOLOGIES, INC. reassignment ADVANCED PROPULSION TECHNOLOGIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SCHMIDT, JASON Z., HOFBAUER, PETER, PRUSINSKI, THOMAS M.
Expired - Fee Related legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18Lubricating arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/14Control of the alternation between or the operation of exhaust drive and other drive of a pump, e.g. dependent on speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/02Drives of pumps; Varying pump drive gear ratio
    • F02B39/08Non-mechanical drives, e.g. fluid drives having variable gear ratio
    • F02B39/10Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/14Lubrication of pumps; Safety measures therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/31Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/315Arrangement of components according to the direction of their main axis or their axis of rotation the main axis being substantially vertical
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the invention relates to the field of turbochargers for use with internal combustion engines. More specifically the invention relates to specific improvements in a lubrication system for a turbocharger as well as the construction of an electrically controlled turbocharger.
  • Turbochargers are frequently employed in association with internal combustion engines to improve engine response under varying loads. Electrically assisted turbochargers provide the added advantage of, reducing transient lag, reducing fuel consumption and lowering emission levels.
  • an electrically assisted turbocharger employs a motor engaged to supply supplemental power to rotate the shaft that extends between the turbine and the compressor. When the engine requires increased demand for intake air and the turbine is not turning at a fast enough speed to provide the demand, the motor is powered to drive the turbine and compressor at a sufficient speed to supply the required air.
  • turbochargers described in the prior art are commonly structured so that the turbine, motor and compressor are mounted on a horizontal shaft. Additionally, the electric motors employed in prior art turbochargers contain magnets that become degraded due to exposure to the extreme heat inherent in such applications.
  • the present invention provides several improvements to an electrically controlled turbocharger unit that result in lower vibration, cooler running temperatures and increased reliability. Such improvements are the result of orienting the unit so that the central shaft containing the turbine and the compressor is mounted to rotate on a substantially vertical axis. This orientation results in the elimination of gravitational effects on the rotating shaft and the elements mounted thereon.
  • an induction motor having its rotor integrally mounted on the shaft that extends between the turbine and the compressor is found to provide highly responsive characteristics and greater endurance to the high temperatures inherent in turbochargers.
  • an improved lubricating system is described to enhance the flow of lubricating fluid through the turbocharger housing and the various bearings in the unit by utilizing air pressure scavenged from the compressor and injected into upper and lower oil reservoirs.
  • FIG. 1 is a cross-sectional plan view of the preferred embodiment of the present invention.
  • FIG. 2 is a 90 degree cross-sectional plan view of the embodiment shown in FIG. 1 .
  • FIG. 3 is a cross-sectional plan view of the preferred embodiment shown in FIGS. 1 and 2 , taken along another vertical plane.
  • FIG. 4 is a block diagram showing the functional inputs and outputs for the electrically controlled turbocharger of the present invention.
  • FIG. 5 is a block diagram showing the flow of air and lubricating fluid into and through an embodiment of the present invention.
  • FIG. 1 the preferred embodiment of an electrically assisted turbocharger unit 100 is depicted in a substantially vertical orientation, intended to be mounted on or in close proximity to an associated internal combustion engine.
  • a turbine housing 102 in shown in the upper portion of FIG. 1 , while a compressor housing 116 is shown in the lower portion.
  • a motor housing 104 is shown as being intermediate the turbine and compressor housings.
  • a turbocharger shaft 114 is at the core of the unit and provides the mechanical drive connection between an exhaust gas turbine rotor 110 and a compressor rotor 119 .
  • an induction motor 132 is provided in motor housing 104 to surround shaft 114 and a motor rotor 136 is formed to be preferably integral with shaft 114 .
  • Turbine housing 102 provides an exhaust gas inlet port 116 that is connected to the exhaust manifold of an associated engine (not shown).
  • Turbine housing 102 contains exhaust gas turbine rotor 110 and a volute 112 through which forced exhaust gas passes.
  • Exhaust gas turbine rotor 110 is shown, in this embodiment, as being integrally forged to shaft 114 .
  • An upper heat shield 109 and an insulation layer 108 are respectively provided between motor housing 104 and turbine housing 102 to resist the conduction of heat from the exhaust gas down to motor housing 104 and all the associated components that may be affected by such temperatures. Since convection heat tends to rise, some of the heat from exhaust gases is dissipated upwards from turbine housing 102 and away from motor housing 104 . In doing so, the rising air caused by the convection heat draws air upwards from below and helps cool the unit. The vertical stacking of the components takes advantage of this phenomenon.
  • Motor housing 104 includes a motor cavity 133 and several passages for the flow of lubricating fluid and scavenged air.
  • Induction motor 132 includes a stator 134 made up of copper wire windings and a rotor (laminate stack and windings) 136 , all within motor cavity 133 .
  • the motor cavity 133 is configured to allow for the unobstructed rotation of the rotor 136 and for the flow of ventilation air scavenged from the compressor.
  • Shaft 114 extends through motor cavity 133 of motor housing 104 and into compressor housing 116 where compressor rotor 119 is attached to shaft 114 by a retainer nut 120 .
  • Compressor housing 116 includes a fresh air intake 118 , compressor rotor 119 , a volute air passage 122 and a compressed air outlet 124 .
  • Shaft 114 is mounted for rotation along its substantially vertically oriented axis on upper bearing 130 and lower bearing 128 .
  • Bearings 130 and 128 are lubricated by the lubrication system and are contained within oil reservoirs 144 and 145 , respectively.
  • Upper oil reservoir 144 is separated from turbine housing 102 by a seal 111 and from motor cavity 133 by a bushing 131 .
  • Lower oil reservoir 145 is the upper part of an oil sump 146 and is separated from compressor housing 116 by a lower compressor seal 121 and from motor cavity 133 by a bushing 129 .
  • An oil inlet 138 is formed in the side of motor housing 104 and is in fluid communication with an upper oil passage 140 and a lower oil passage 142 .
  • Upper oil passage 140 extends upwards to allow the delivery of oil to upper bearing 130 at its upper bearing oil injection port 141 .
  • Lower oil passage 142 extends laterally through motor housing 104 towards lower bearing 128 to allow the delivery of oil to the lower bearing 128 at its lower bearing oil injection port 143 .
  • Upper oil reservoir 144 is in fluid communication with drain passage 149 that is in turn connected to a drain outlet 148 .
  • lower oil reservoir 145 is in fluid communication with an oil sump 146 that is formed between motor housing 104 and compressor housing 116 .
  • Oil sump 146 is in fluid communication with a sump drain 147 that is connected to drain outlet 148 .
  • FIG. 2 a 90 degree cross-sectional plan view of the turbocharger embodiment shown in FIG. 1 is presented. This view is taken along the vertical axis A-A.
  • the left side of FIG. 2 illustrates substantially the same components and features shown in FIG. 1 , while the right side is a 90 degree rotation and shows the air injection portion of the lubricating system.
  • a scavenged air inlet 150 is shown in communication with compressor volute passage 122 .
  • a scavenged air passage 152 is in fluid communication with air inlet 150 and opens into motor cavity 133 .
  • An air outlet passage 154 provides a path for air to flow from motor cavity 133 to upper oil reservoir 144 .
  • Another air outlet passage 156 is formed at the lower portion of motor cavity 133 (added to left side of FIG. 2 ) in fluid communication with lower oil reservoir 145 to allow for the scavenged air to escape from the motor cavity 133 .
  • FIG. 3 one of three electrical interconnections is illustrated for the turbocharger embodiment 100 .
  • the interconnection is between a stud terminal 160 , mounted on motor housing 104 , and stator windings 134 through a lead wire 162 .
  • the electrically controlled turbocharger is shown in its generic sense as receiving exhaust gas flowing from the associated engine and controlled electrical power from an associated controller.
  • the controller provides alternating current or pulse width variable power to the electric induction motor to control its speed when required during cold start, other low idle conditions or acceleration demands in which the exhaust gas output from the engine is insufficient to cause the turbocharger to supply adequate amounts of fresh air to the intake manifold of the engine.
  • the controller responsively reduces power to the induction motor until the electric motor assist is no longer needed.
  • the lubrication system of the preferred embodiment functions in accordance with the flow diagram of FIG. 5 , with reference to the components shown in FIGS. 1 and 2 .
  • the oil is provided to oil inlet 138 from an auxiliary pump at a predetermined pressure and volume. It has been found that during cold starts or cold weather, the oil needs assistance to flow through the passages in an efficient manner.
  • the location of the oil sump 146 at a level below the drain outlet requires positive pressure to keep the level below a predetermined level at all temperatures.
  • the lubricating system utilizes pressurized scavenged air from compressor volute 122 to perform several tasks. First, the scavenged air flows into motor cavity 133 and provides a limited amount of ventilation to induction motor 132 .
  • the air in motor cavity 133 creates a positive pressure against upper motor cavity bushing 131 and lower motor cavity bushing 129 to prevent oil in the opposing reservoirs from entering motor cavity 133 .
  • the air exits from motor cavity 133 through air outlet 154 and enters upper oil reservoir 144 it provides additional pressure to the oil that has entered that same reservoir to drive the oil into the drain passage 149 .
  • the air that enters lower oil reservoir 145 from motor cavity 133 through air outlet 156 blows past the oil collected in the sump towards the drain oil outlet 148 and creates a vacuum. This vacuum in turn causes oil to be drawn from the sump and maintain the oil level therein at a desired level.

Abstract

An electrically controlled turbocharger having a substantially vertically oriented shaft interconnecting a turbine and a compressor. The vertical orientation serves to eliminate the effects of gravity on the rotating components. Placing the turbine vertically above the motor and compressor and provides additional cooling through convection of heat produced by hot exhaust gas flowing through the turbine. A lubricating system utilizes scavenged air from the compressor to draw lubricating oil through internal passages of the motor housing to maintain a desirable oil sump level, ventilate the auxiliary induction motor, and provide pressure to the oil seals of the motor cavity.

Description

    RELATED APPLICATION
  • This application and the claimed subject matter is supported by Applicant's provisional application Ser. No. 60/669,598 to TURBOCHARGER, filed Apr. 9, 2005 and the benefit to priority of that date is hereby claimed.
  • BACKGROUND
  • 1. Field of the Invention
  • The invention relates to the field of turbochargers for use with internal combustion engines. More specifically the invention relates to specific improvements in a lubrication system for a turbocharger as well as the construction of an electrically controlled turbocharger.
  • 2. Description of the Prior Art
  • Turbochargers are frequently employed in association with internal combustion engines to improve engine response under varying loads. Electrically assisted turbochargers provide the added advantage of, reducing transient lag, reducing fuel consumption and lowering emission levels. Typically, an electrically assisted turbocharger employs a motor engaged to supply supplemental power to rotate the shaft that extends between the turbine and the compressor. When the engine requires increased demand for intake air and the turbine is not turning at a fast enough speed to provide the demand, the motor is powered to drive the turbine and compressor at a sufficient speed to supply the required air.
  • Such turbochargers described in the prior art are commonly structured so that the turbine, motor and compressor are mounted on a horizontal shaft. Additionally, the electric motors employed in prior art turbochargers contain magnets that become degraded due to exposure to the extreme heat inherent in such applications.
  • SUMMARY OF THE INVENTION
  • The present invention provides several improvements to an electrically controlled turbocharger unit that result in lower vibration, cooler running temperatures and increased reliability. Such improvements are the result of orienting the unit so that the central shaft containing the turbine and the compressor is mounted to rotate on a substantially vertical axis. This orientation results in the elimination of gravitational effects on the rotating shaft and the elements mounted thereon. In addition, an induction motor having its rotor integrally mounted on the shaft that extends between the turbine and the compressor is found to provide highly responsive characteristics and greater endurance to the high temperatures inherent in turbochargers. Further, an improved lubricating system is described to enhance the flow of lubricating fluid through the turbocharger housing and the various bearings in the unit by utilizing air pressure scavenged from the compressor and injected into upper and lower oil reservoirs.
  • It is an object of the present invention to provide a vertically oriented turbocharger that reduces and therefore improves the vibration characteristics of the turbo shaft at high speed rotations.
  • It is another object of the present invention to provide an improved electrically controlled turbocharger that utilizes an induction motor for driving the compressor when exhaust gas flow from the associated internal combustion engine is insufficient to provide the necessary drive power.
  • It is a further object of the invention to provide an improved lubricating system for vertically oriented turbochargers that is effective to provide lubricating fluid to the vertically spaced shaft bearings.
  • It is a still further object of the present invention to provide improved cooling for an electrically controlled turbocharger through the use of air scavenged from the compressor and ducted into the motor and lubricating system that circulates lubricating fluid through the housing of the turbocharger.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a cross-sectional plan view of the preferred embodiment of the present invention.
  • FIG. 2 is a 90 degree cross-sectional plan view of the embodiment shown in FIG. 1.
  • FIG. 3 is a cross-sectional plan view of the preferred embodiment shown in FIGS. 1 and 2, taken along another vertical plane.
  • FIG. 4 is a block diagram showing the functional inputs and outputs for the electrically controlled turbocharger of the present invention.
  • FIG. 5 is a block diagram showing the flow of air and lubricating fluid into and through an embodiment of the present invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • In FIG. 1, the preferred embodiment of an electrically assisted turbocharger unit 100 is depicted in a substantially vertical orientation, intended to be mounted on or in close proximity to an associated internal combustion engine.
  • In this embodiment, a turbine housing 102 in shown in the upper portion of FIG. 1, while a compressor housing 116 is shown in the lower portion. A motor housing 104 is shown as being intermediate the turbine and compressor housings.
  • A turbocharger shaft 114 is at the core of the unit and provides the mechanical drive connection between an exhaust gas turbine rotor 110 and a compressor rotor 119. In this case an induction motor 132 is provided in motor housing 104 to surround shaft 114 and a motor rotor 136 is formed to be preferably integral with shaft 114.
  • Turbine housing 102 provides an exhaust gas inlet port 116 that is connected to the exhaust manifold of an associated engine (not shown). Turbine housing 102 contains exhaust gas turbine rotor 110 and a volute 112 through which forced exhaust gas passes. Exhaust gas turbine rotor 110 is shown, in this embodiment, as being integrally forged to shaft 114.
  • An upper heat shield 109 and an insulation layer 108 are respectively provided between motor housing 104 and turbine housing 102 to resist the conduction of heat from the exhaust gas down to motor housing 104 and all the associated components that may be affected by such temperatures. Since convection heat tends to rise, some of the heat from exhaust gases is dissipated upwards from turbine housing 102 and away from motor housing 104. In doing so, the rising air caused by the convection heat draws air upwards from below and helps cool the unit. The vertical stacking of the components takes advantage of this phenomenon.
  • Motor housing 104 includes a motor cavity 133 and several passages for the flow of lubricating fluid and scavenged air. Induction motor 132 includes a stator 134 made up of copper wire windings and a rotor (laminate stack and windings) 136, all within motor cavity 133. The motor cavity 133 is configured to allow for the unobstructed rotation of the rotor 136 and for the flow of ventilation air scavenged from the compressor. Shaft 114 extends through motor cavity 133 of motor housing 104 and into compressor housing 116 where compressor rotor 119 is attached to shaft 114 by a retainer nut 120.
  • Compressor housing 116 includes a fresh air intake 118, compressor rotor 119, a volute air passage 122 and a compressed air outlet 124.
  • Shaft 114 is mounted for rotation along its substantially vertically oriented axis on upper bearing 130 and lower bearing 128. Bearings 130 and 128 are lubricated by the lubrication system and are contained within oil reservoirs 144 and 145, respectively. Upper oil reservoir 144 is separated from turbine housing 102 by a seal 111 and from motor cavity 133 by a bushing 131. Lower oil reservoir 145 is the upper part of an oil sump 146 and is separated from compressor housing 116 by a lower compressor seal 121 and from motor cavity 133 by a bushing 129.
  • An oil inlet 138 is formed in the side of motor housing 104 and is in fluid communication with an upper oil passage 140 and a lower oil passage 142. Upper oil passage 140 extends upwards to allow the delivery of oil to upper bearing 130 at its upper bearing oil injection port 141. Lower oil passage 142 extends laterally through motor housing 104 towards lower bearing 128 to allow the delivery of oil to the lower bearing 128 at its lower bearing oil injection port 143.
  • Upper oil reservoir 144 is in fluid communication with drain passage 149 that is in turn connected to a drain outlet 148. At the lower end of the unit, lower oil reservoir 145 is in fluid communication with an oil sump 146 that is formed between motor housing 104 and compressor housing 116. Oil sump 146 is in fluid communication with a sump drain 147 that is connected to drain outlet 148.
  • In FIG. 2, a 90 degree cross-sectional plan view of the turbocharger embodiment shown in FIG. 1 is presented. This view is taken along the vertical axis A-A. The left side of FIG. 2 illustrates substantially the same components and features shown in FIG. 1, while the right side is a 90 degree rotation and shows the air injection portion of the lubricating system. A scavenged air inlet 150 is shown in communication with compressor volute passage 122. A scavenged air passage 152 is in fluid communication with air inlet 150 and opens into motor cavity 133. An air outlet passage 154 provides a path for air to flow from motor cavity 133 to upper oil reservoir 144. Another air outlet passage 156 is formed at the lower portion of motor cavity 133 (added to left side of FIG. 2) in fluid communication with lower oil reservoir 145 to allow for the scavenged air to escape from the motor cavity 133.
  • In FIG. 3, one of three electrical interconnections is illustrated for the turbocharger embodiment 100. The interconnection is between a stud terminal 160, mounted on motor housing 104, and stator windings 134 through a lead wire 162.
  • In FIG. 4, the electrically controlled turbocharger is shown in its generic sense as receiving exhaust gas flowing from the associated engine and controlled electrical power from an associated controller. In this case, the controller provides alternating current or pulse width variable power to the electric induction motor to control its speed when required during cold start, other low idle conditions or acceleration demands in which the exhaust gas output from the engine is insufficient to cause the turbocharger to supply adequate amounts of fresh air to the intake manifold of the engine. As the engine increases its speed and produces more exhaust gas to drive the turbine, the controller responsively reduces power to the induction motor until the electric motor assist is no longer needed.
  • The lubrication system of the preferred embodiment functions in accordance with the flow diagram of FIG. 5, with reference to the components shown in FIGS. 1 and 2. In this system, the oil is provided to oil inlet 138 from an auxiliary pump at a predetermined pressure and volume. It has been found that during cold starts or cold weather, the oil needs assistance to flow through the passages in an efficient manner. In addition, the location of the oil sump 146 at a level below the drain outlet requires positive pressure to keep the level below a predetermined level at all temperatures. The lubricating system utilizes pressurized scavenged air from compressor volute 122 to perform several tasks. First, the scavenged air flows into motor cavity 133 and provides a limited amount of ventilation to induction motor 132. Second, the air in motor cavity 133 creates a positive pressure against upper motor cavity bushing 131 and lower motor cavity bushing 129 to prevent oil in the opposing reservoirs from entering motor cavity 133. Third, as the air exits from motor cavity 133 through air outlet 154 and enters upper oil reservoir 144, it provides additional pressure to the oil that has entered that same reservoir to drive the oil into the drain passage 149. Fourth, the air that enters lower oil reservoir 145 from motor cavity 133 through air outlet 156 blows past the oil collected in the sump towards the drain oil outlet 148 and creates a vacuum. This vacuum in turn causes oil to be drawn from the sump and maintain the oil level therein at a desired level.
  • It should be understood that the foregoing description of the embodiments is merely illustrative of many possible implementations of the present invention and is not intended to be exhaustive.

Claims (18)

1. A turbocharger comprising:
a turbine within a turbine housing configured to be rotationally driven by exhaust gases produced by an internal combustion engine;
a compressor within a compressor housing configured to be rotationally driven by said turbine to supply compressed air to an internal combustion engine;
a turbo shaft oriented along a substantially vertical axis interconnecting said turbine and said compressor to provide said rotational drive to said compressor along said substantially vertical axis;
an induction motor within a motor housing located between said turbine and compressor housings configured to have a rotor integral with said turbo shaft to provide controlled auxiliary rotational driving force to said shaft and said compressor.
2. A turbocharger as in claim 1, wherein said turbo shaft is vertically mounted in said motor housing by upper and lower bearings and said motor housing contains passages within said motor housing for allowing the flow of lubricating oil from an oil inlet to an oil outlet and to lubricate said upper and lower bearings.
3. A turbocharger as in claim 2, wherein said motor housing contains a motor cavity which provides for unobstructed rotation of said rotor and said motor housing and said turbocharger further includes an air scavenging passage between said compressor and said motor cavity to provide relatively cooled air from said compressor to ventilate said motor.
4. A turbocharger as in claim 3, wherein said scavenged air in said motor cavity under pressure from said compressor acts to keep lubricating oil from migrating through said bearings into said motor cavity.
5. A turbocharger as in claim 3, wherein said motor housing further contains an oil sump adjacent said lower bearing, said oil flow passages are in communication with said oil sump and said sump is in communication with said oil outlet.
6. A turbocharger as in claim 5, wherein said motor housing contains an outlet air passage in communication between said motor cavity and said sump to allow said scavenged air to escape said motor cavity and assist the removal of oil collected in said sump to said oil outlet.
7. A turbocharger as in claim 1, wherein said turbine is mounted vertically above said motor and said compressor to allow radiate heat from the turbine, due to exhaust gasses flowing in the turbine, to cause convection flow of ambient air to be drawn over the turbocharger for additional cooling effect.
8. A turbocharger as in claim 1, wherein said motor housing contains a motor cavity which provides for unobstructed rotation of said rotor and said motor housing and said turbocharger further includes an air scavenging passage between said compressor and said motor cavity to provide relatively cooled air from said compressor to ventilate said motor.
9. A turbocharger as in claim 8, wherein said oil passages comprise a first oil passage that extends from said oil inlet to said upper bearing and a second oil passage extends from said oil inlet to a lower bearing.
10. A turbocharger s in claim 9, and said motor housing further includes an upper reservoir in communication with said upper bearing and a lower reservoir in communication with said lower bearing, and oil from said upper bearing flows to said upper reservoir and from said lower bearing to said lower reservoir.
11. A turbocharger as in claim 10, wherein said scavenged air in said motor cavity under pressure from said compressor functions to keep lubricating oil from migrating through said bearings into said motor cavity.
12. A turbocharger as in claim 10, wherein said motor housing further contains an oil sump adjacent said lower bearing and in communication to receive oil from said lower reservoir, said oil passages comprise a third oil passage that extends from said upper reservoir to said oil outlet and a fourth oil passage that extends from said oil sump to said oil outlet.
13. A turbocharger s in claim 12, wherein said motor housing contains an outlet air passage in communication between said motor cavity and said sump to allow said scavenged air to escape said motor cavity under pressure and assist the forced removal of oil collected in said sump through said fourth oil passage and said oil outlet.
14. A turbocharger comprising:
a turbine within a turbine housing configured to be rotationally driven by exhaust gases produced by an internal combustion engine;
a compressor within a compressor housing configured to be rotationally driven by said turbine to supply compressed air to an internal combustion engine;
a turbo shaft interconnecting said turbine and said compressor to provide said rotational drive to said compressor along said an axis;
an induction motor, within a motor housing containing a motor cavity, located between said turbine and compressor housings configured to have a rotor integral with said turbo shaft to provide controlled auxiliary rotational driving force to said shaft and said compressor; wherein said rotor is contained within said motor cavity for unobstructed rotation therein; and an air scavenging passage between said compressor and said motor cavity to provide scavenged air to said motor cavity.
15. A turbocharger as in claim 14, wherein said turbo shaft is vertically mounted in said motor housing by upper and lower bearings and said motor housing contains passages within said motor housing for allowing the flow of lubricating oil from an oil inlet to an oil outlet and to lubricate said upper and lower bearings.
16. A turbocharger as in claim 15, wherein said motor housing further contains an oil sump adjacent said lower bearing, said oil flow passages are in communication with said oil sump and said sump is in communication with said oil outlet.
17. A turbocharger as in claim 16, wherein said motor housing contains an outlet air passage in communication between said motor cavity and said sump to allow said scavenged air to escape said motor cavity and assist the removal of oil collected in said sump to said oil outlet.
18. A turbocharger as in claim 14, wherein said scavenged air in said motor cavity under pressure from said compressor functions to keep lubricating oil from migrating into said motor cavity.
US11/399,775 2005-04-09 2006-04-07 Turbocharger Expired - Fee Related US7360361B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/399,775 US7360361B2 (en) 2005-04-09 2006-04-07 Turbocharger

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US66959805P 2005-04-09 2005-04-09
US11/399,775 US7360361B2 (en) 2005-04-09 2006-04-07 Turbocharger

Publications (2)

Publication Number Publication Date
US20060225419A1 true US20060225419A1 (en) 2006-10-12
US7360361B2 US7360361B2 (en) 2008-04-22

Family

ID=37081822

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/399,775 Expired - Fee Related US7360361B2 (en) 2005-04-09 2006-04-07 Turbocharger

Country Status (1)

Country Link
US (1) US7360361B2 (en)

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060123783A1 (en) * 2003-04-15 2006-06-15 Noelle Philippe Electric motor cartridge for an electrically assisted turbocharger
US20100043431A1 (en) * 2006-11-01 2010-02-25 Borgwarner Inc. Turbine heat shield assembly
US20100218499A1 (en) * 2006-06-02 2010-09-02 Ihi Corporation Motor-driven supercharger
US20100218498A1 (en) * 2006-06-02 2010-09-02 Ihi Corporation Motor-driven supercharger
US20100247343A1 (en) * 2006-08-18 2010-09-30 Ihi Corporation Motor-driven supercharger
US20100247342A1 (en) * 2006-08-18 2010-09-30 Ihi Corporation Motor-driven supercharger
US20100287932A1 (en) * 2009-05-14 2010-11-18 Mitsubishi Electric Corporation Internal-combustion-engine control apparatus
US20100310366A1 (en) * 2008-01-28 2010-12-09 Ihi Corporation Supercharger
US8157543B2 (en) 2006-03-23 2012-04-17 Ihi Corporation High-speed rotating shaft of supercharger
CN102797553A (en) * 2011-05-25 2012-11-28 通用汽车环球科技运作有限责任公司 Engine assembly including turbocharger
WO2013122857A1 (en) * 2012-02-17 2013-08-22 Borgwarner Inc. Multi-segment turbocharger bearing housing and methods therefor
WO2013180960A2 (en) * 2012-05-29 2013-12-05 Borgwarner Inc. Exhaust-gas turbocharger
US20140056721A1 (en) * 2012-08-24 2014-02-27 Ecomotors, Inc. Shield and Coolant Guide for an Electric Machine
US20140056726A1 (en) * 2012-08-24 2014-02-27 Ecomotors, Inc. Cooling Stator Windings of an Electric Machine
US20140064917A1 (en) * 2012-09-06 2014-03-06 Weir Minerals Australia, Ltd. Hydraulic Motor-Driven Bearing Lubrication System For A Centrifugal Pump
WO2014074433A1 (en) * 2012-11-12 2014-05-15 Borgwarner Inc. Supplemental air cooling system and air pressure oil sealing system for electrical turbocompound machine
US20140147306A1 (en) * 2011-06-08 2014-05-29 Mitsubishi Heavy Industries, Ltd. Structure and method for adjusting balance of turbocharging device incorporating electric motor
US20140301827A1 (en) * 2013-04-09 2014-10-09 Abb Turbo Systems Ag Housing of a radial compressor
US20150056064A1 (en) * 2012-03-30 2015-02-26 Taiho Kogyo Co., Ltd. Turbocharger bearing housing
US20160032817A1 (en) * 2014-08-04 2016-02-04 Jeffrey J. Buschur Power conversion device
US9470231B2 (en) 2012-01-06 2016-10-18 Borgwarner Inc. Electrically assisted turbocharger
EP3159507A1 (en) * 2015-10-20 2017-04-26 BorgWarner Inc. Oil supply conduit through stator lamination stack for electrified turbocharger
CN108561222A (en) * 2018-04-04 2018-09-21 江苏凯迪航控系统股份有限公司 Having electronic quickly starts the turbocharger of separate structure
US20190284992A1 (en) * 2018-03-14 2019-09-19 Borgwarner Inc. Cooling and Lubrication System for a Turbocharger
US10851689B2 (en) * 2018-06-13 2020-12-01 Rolls-Royce Corporation Drainage path for a bearing sump in a vertically oriented turbine engine
DE102012206650B4 (en) 2012-04-23 2024-03-28 Ford Global Technologies, Llc Turbocharger arrangement for an internal combustion engine

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4539487B2 (en) * 2005-08-05 2010-09-08 株式会社Ihi Supercharger with electric motor
JP4591828B2 (en) * 2005-08-22 2010-12-01 株式会社Ihi Supercharger with electric motor
DE602006020239D1 (en) * 2006-01-24 2011-04-07 Ihi Corp Motor powered charging
EP1813782B1 (en) 2006-01-26 2009-08-05 IHI Corporation Turbo-supercharger
JP4720783B2 (en) * 2007-05-09 2011-07-13 日産自動車株式会社 Supercharger lubrication device
PL2158387T3 (en) * 2007-05-24 2013-12-31 Lindenmaier Gmbh Compressor assembly
JP2009013966A (en) * 2007-07-09 2009-01-22 Ihi Corp Supercharger with electric motor
KR101182122B1 (en) * 2008-04-08 2012-09-13 가부시키가이샤 아이에이치아이 Turbocharger
DE102008055632B4 (en) * 2008-11-03 2012-05-16 Aerodyn Engineering Gmbh Method for lubricating a gearbox
US20110022289A1 (en) * 2009-07-27 2011-01-27 Ecomotors International, Inc. Method of controlling an electrically assisted turbocharger
US8958971B2 (en) 2009-07-27 2015-02-17 Ecomotors, Inc. System and method to control an electronically-controlled turbocharger
IN2014DN07367A (en) * 2012-02-20 2015-04-24 Borgwarner Inc
GB2502269B (en) 2012-05-21 2014-12-03 Perkins Engines Co Ltd Method and apparatus for controlling the starting of a forced induction internal combustion engine
US9003793B2 (en) * 2013-05-31 2015-04-14 GM Global Technology Operations LLC Turbocharger assembly with compressed air cooled bearings
JP6794922B2 (en) * 2017-05-12 2020-12-02 株式会社豊田自動織機 Electric supercharger
FR3074622B1 (en) 2017-12-04 2021-07-30 Ifp Energies Now DEVICE FOR COMPRESSION OF A FLUID DRIVEN BY AN ELECTRIC MACHINE WITH A ROTOR SHAFT HAVING AN AMAGNETIC FRET
FR3078205B1 (en) 2018-02-16 2020-02-28 IFP Energies Nouvelles ELECTRIC MACHINE WITH STATOR GRID COMPRISING AERODYNAMIC APPENDICES
FR3078844B1 (en) 2018-03-08 2021-10-08 Ifp Energies Now DOUBLE-FLOW ELECTRIC MACHINE
FR3089712B1 (en) * 2018-12-11 2023-03-10 Ifp Energies Now Electric machine stator with a ring formed by a plurality of stator segments
FR3092448B1 (en) 2019-02-04 2021-01-15 Ifp Energies Now Device for compressing a fluid driven by an electric machine with a rotor equipped with a solid cylindrical magnet
FR3092449B1 (en) 2019-02-04 2022-01-14 Ifp Energies Now Device for compressing a fluid driven by an electric machine with compression shaft passing through the rotor
DK3745559T3 (en) * 2019-05-27 2022-06-07 Magnax Bv Stator til aksialfluxmaskine
FR3101208B1 (en) 2019-09-23 2023-06-30 Ifp Energies Now Hybrid transient magnet rotor
DE102021126406A1 (en) 2021-10-12 2023-04-13 Ihi Charging Systems International Gmbh Electrically assisted exhaust gas turbocharger, drive unit with an electrically assisted exhaust gas turbocharger and method for an electrically assisted exhaust gas turbocharger

Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1428925A (en) * 1920-06-29 1922-09-12 Carl C Thomas Supercharger for internal-combustion engines
US2234777A (en) * 1938-02-16 1941-03-11 Gen Electric Lubricating system
US2296703A (en) * 1939-01-21 1942-09-22 Bristol Aeroplane Co Ltd Gas turbine
US2646210A (en) * 1951-05-05 1953-07-21 Eberspaecher J Turbocompressor
US2702093A (en) * 1949-10-21 1955-02-15 Bendix Aviat Corp Lubricating system for high-speed machines
US3382670A (en) * 1966-12-01 1968-05-14 Gen Electric Gas turbine engine lubrication system
US3687233A (en) * 1970-07-23 1972-08-29 Garrett Corp Integral lubrication system
US3895620A (en) * 1970-09-08 1975-07-22 Berry W Foster Engine and gas generator
US4009972A (en) * 1975-07-10 1977-03-01 Wallace-Murray Corporation Turbocharger lubrication and exhaust system
US4235484A (en) * 1979-02-22 1980-11-25 Wallace Murray Corporation Bearing carrier with integral lubricating sealing features
US4253031A (en) * 1978-05-27 1981-02-24 Robert Bosch Gmbh Directly driven dynamo electric machine-gas turbine generator structure
US4364717A (en) * 1978-07-03 1982-12-21 Barmag Barmer Maschinenfabrik Ag Exhaust gas turbocharger
US4525995A (en) * 1983-04-04 1985-07-02 Williams International Corporation Oil scavening system for gas turbine engine
US5605045A (en) * 1995-09-18 1997-02-25 Turbodyne Systems, Inc. Turbocharging system with integral assisting electric motor and cooling system therefor
US6050780A (en) * 1995-10-25 2000-04-18 Ishikawajima-Harima Heavy Industries Co., Ltd. Method for driving a high speed compressor
US6102672A (en) * 1997-09-10 2000-08-15 Turbodyne Systems, Inc. Motor-driven centrifugal air compressor with internal cooling airflow
US6257834B1 (en) * 1998-02-10 2001-07-10 Asea Brown Boveri Ag Method and arrangement for the indirect cooling of the flow in radial gaps formed between rotors and stators of turbomachines
US6609375B2 (en) * 2001-09-14 2003-08-26 Honeywell International Inc. Air cooling system for electric assisted turbocharger
US7056103B2 (en) * 2004-03-05 2006-06-06 Honeywell International, Inc. Method and apparatus for cooling turbomachinery components

Patent Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1428925A (en) * 1920-06-29 1922-09-12 Carl C Thomas Supercharger for internal-combustion engines
US2234777A (en) * 1938-02-16 1941-03-11 Gen Electric Lubricating system
US2296703A (en) * 1939-01-21 1942-09-22 Bristol Aeroplane Co Ltd Gas turbine
US2702093A (en) * 1949-10-21 1955-02-15 Bendix Aviat Corp Lubricating system for high-speed machines
US2646210A (en) * 1951-05-05 1953-07-21 Eberspaecher J Turbocompressor
US3382670A (en) * 1966-12-01 1968-05-14 Gen Electric Gas turbine engine lubrication system
US3687233A (en) * 1970-07-23 1972-08-29 Garrett Corp Integral lubrication system
US3895620A (en) * 1970-09-08 1975-07-22 Berry W Foster Engine and gas generator
US4009972A (en) * 1975-07-10 1977-03-01 Wallace-Murray Corporation Turbocharger lubrication and exhaust system
US4253031A (en) * 1978-05-27 1981-02-24 Robert Bosch Gmbh Directly driven dynamo electric machine-gas turbine generator structure
US4364717A (en) * 1978-07-03 1982-12-21 Barmag Barmer Maschinenfabrik Ag Exhaust gas turbocharger
US4235484A (en) * 1979-02-22 1980-11-25 Wallace Murray Corporation Bearing carrier with integral lubricating sealing features
US4525995A (en) * 1983-04-04 1985-07-02 Williams International Corporation Oil scavening system for gas turbine engine
US5605045A (en) * 1995-09-18 1997-02-25 Turbodyne Systems, Inc. Turbocharging system with integral assisting electric motor and cooling system therefor
US6050780A (en) * 1995-10-25 2000-04-18 Ishikawajima-Harima Heavy Industries Co., Ltd. Method for driving a high speed compressor
US6102672A (en) * 1997-09-10 2000-08-15 Turbodyne Systems, Inc. Motor-driven centrifugal air compressor with internal cooling airflow
US6257834B1 (en) * 1998-02-10 2001-07-10 Asea Brown Boveri Ag Method and arrangement for the indirect cooling of the flow in radial gaps formed between rotors and stators of turbomachines
US6609375B2 (en) * 2001-09-14 2003-08-26 Honeywell International Inc. Air cooling system for electric assisted turbocharger
US7056103B2 (en) * 2004-03-05 2006-06-06 Honeywell International, Inc. Method and apparatus for cooling turbomachinery components

Cited By (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7458214B2 (en) * 2003-04-15 2008-12-02 Honeywell International, Inc. Electric motor cartridge for an electrically assisted turbocharger
US20060123783A1 (en) * 2003-04-15 2006-06-15 Noelle Philippe Electric motor cartridge for an electrically assisted turbocharger
US8157543B2 (en) 2006-03-23 2012-04-17 Ihi Corporation High-speed rotating shaft of supercharger
US20100218499A1 (en) * 2006-06-02 2010-09-02 Ihi Corporation Motor-driven supercharger
US20100218498A1 (en) * 2006-06-02 2010-09-02 Ihi Corporation Motor-driven supercharger
US8001781B2 (en) 2006-06-02 2011-08-23 Ihi Corporation Motor-driven supercharger
US8096126B2 (en) * 2006-06-02 2012-01-17 Ihi Corporation Motor-driven supercharger
US8152489B2 (en) 2006-08-18 2012-04-10 Ihi Corporation Motor-driven supercharger
US20100247343A1 (en) * 2006-08-18 2010-09-30 Ihi Corporation Motor-driven supercharger
US20100247342A1 (en) * 2006-08-18 2010-09-30 Ihi Corporation Motor-driven supercharger
US8157544B2 (en) 2006-08-18 2012-04-17 Ihi Corporation Motor driven supercharger with motor/generator cooling efficacy
US8376721B2 (en) * 2006-11-01 2013-02-19 Borgwarner Inc. Turbine heat shield assembly
US20100043431A1 (en) * 2006-11-01 2010-02-25 Borgwarner Inc. Turbine heat shield assembly
US20100310366A1 (en) * 2008-01-28 2010-12-09 Ihi Corporation Supercharger
US8622691B2 (en) 2008-01-28 2014-01-07 Ihi Corporation Supercharger
US20100287932A1 (en) * 2009-05-14 2010-11-18 Mitsubishi Electric Corporation Internal-combustion-engine control apparatus
CN102797553A (en) * 2011-05-25 2012-11-28 通用汽车环球科技运作有限责任公司 Engine assembly including turbocharger
US20120301278A1 (en) * 2011-05-25 2012-11-29 GM Global Technology Operations LLC Engine assembly including turbocharger
US8544268B2 (en) * 2011-05-25 2013-10-01 GM Global Technology Operations LLC Engine assembly including turbocharger
US20140147306A1 (en) * 2011-06-08 2014-05-29 Mitsubishi Heavy Industries, Ltd. Structure and method for adjusting balance of turbocharging device incorporating electric motor
US9470231B2 (en) 2012-01-06 2016-10-18 Borgwarner Inc. Electrically assisted turbocharger
US10670029B2 (en) 2012-02-17 2020-06-02 Borgwarner Inc. Multi-segment turbocharger bearing housing and methods therefor
WO2013122857A1 (en) * 2012-02-17 2013-08-22 Borgwarner Inc. Multi-segment turbocharger bearing housing and methods therefor
CN104145099A (en) * 2012-02-17 2014-11-12 博格华纳公司 Multi-segment turbocharger bearing housing and methods therefor
US20150056064A1 (en) * 2012-03-30 2015-02-26 Taiho Kogyo Co., Ltd. Turbocharger bearing housing
US9790956B2 (en) * 2012-03-30 2017-10-17 Taiho Kogyo Co., Ltd. Turbocharger bearing housing
DE102012206650B4 (en) 2012-04-23 2024-03-28 Ford Global Technologies, Llc Turbocharger arrangement for an internal combustion engine
WO2013180960A3 (en) * 2012-05-29 2014-02-27 Borgwarner Inc. Exhaust-gas turbocharger
WO2013180960A2 (en) * 2012-05-29 2013-12-05 Borgwarner Inc. Exhaust-gas turbocharger
CN104302889A (en) * 2012-05-29 2015-01-21 博格华纳公司 Exhaust-gas turbocharger
US10001137B2 (en) 2012-05-29 2018-06-19 Borgwarner Inc. Exhaust-gas turbocharger
US20140056721A1 (en) * 2012-08-24 2014-02-27 Ecomotors, Inc. Shield and Coolant Guide for an Electric Machine
US20140056726A1 (en) * 2012-08-24 2014-02-27 Ecomotors, Inc. Cooling Stator Windings of an Electric Machine
US9401630B2 (en) * 2012-08-24 2016-07-26 Ecomotors, Inc. Cooling stator windings of an electric machine
US20140064917A1 (en) * 2012-09-06 2014-03-06 Weir Minerals Australia, Ltd. Hydraulic Motor-Driven Bearing Lubrication System For A Centrifugal Pump
US9388820B2 (en) * 2012-09-06 2016-07-12 Weir Minerals Australia, Ltd. Hydraulic motor-driven bearing lubrication system for a centrifugal pump
US9835172B2 (en) 2012-11-12 2017-12-05 Borgwarner Inc. Supplemental air cooling system and air pressure oil sealing system for electrical turbocompound machine
WO2014074433A1 (en) * 2012-11-12 2014-05-15 Borgwarner Inc. Supplemental air cooling system and air pressure oil sealing system for electrical turbocompound machine
US9541095B2 (en) * 2013-04-09 2017-01-10 Abb Turbo Systems Ag Housing of a radial compressor
US20140301827A1 (en) * 2013-04-09 2014-10-09 Abb Turbo Systems Ag Housing of a radial compressor
US9915192B2 (en) * 2014-08-04 2018-03-13 Jeffrey J. Buschur Power conversion device
US20160032817A1 (en) * 2014-08-04 2016-02-04 Jeffrey J. Buschur Power conversion device
EP3159507A1 (en) * 2015-10-20 2017-04-26 BorgWarner Inc. Oil supply conduit through stator lamination stack for electrified turbocharger
US10119459B2 (en) 2015-10-20 2018-11-06 Borgwarner Inc. Oil supply conduit through stator lamination stack for electrified turbocharger
US10598084B2 (en) * 2018-03-14 2020-03-24 Borgwarner Inc. Cooling and lubrication system for a turbocharger
US20190284992A1 (en) * 2018-03-14 2019-09-19 Borgwarner Inc. Cooling and Lubrication System for a Turbocharger
CN108561222A (en) * 2018-04-04 2018-09-21 江苏凯迪航控系统股份有限公司 Having electronic quickly starts the turbocharger of separate structure
US10851689B2 (en) * 2018-06-13 2020-12-01 Rolls-Royce Corporation Drainage path for a bearing sump in a vertically oriented turbine engine

Also Published As

Publication number Publication date
US7360361B2 (en) 2008-04-22

Similar Documents

Publication Publication Date Title
US7360361B2 (en) Turbocharger
US7946118B2 (en) Cooling an electrically controlled turbocharger
US8393152B2 (en) Electric supercharger
US5638796A (en) Electric supercharger
US5605045A (en) Turbocharging system with integral assisting electric motor and cooling system therefor
CN100557209C (en) The pressure-increasing machine of charged motivation
DE112010000875B4 (en) Improvements in an electrically controlled turbocharger
CN101715624B (en) Two-stage cooling fan for an electric generator
JP4043947B2 (en) Electric drive fluid compressor
CN1281535A (en) Motor-driven centrifugal air compressor with internal cooling airflow
US10598084B2 (en) Cooling and lubrication system for a turbocharger
US11542958B2 (en) Exhaust turbocharger
US20050069434A1 (en) Submerged pump having a bearing lubricated by discharged fluid
CN110905653B (en) Two-stroke aviation piston engine supercharger
US20060032261A1 (en) Thermal management of a gas turbine bearing compartment utilizing separate lubrication and cooling circuits
JP2008121466A (en) Motor-driven supercharger
US11105257B2 (en) Liquid-cooled power electronics assembly for electrically-actuated turbochargers
JP2008128112A (en) Electrically-driven supercharger
US20160208675A1 (en) Cooling system, device and method for a vehicle
JP2008295192A (en) Rotary electric machine
JP2006090274A (en) Turbocharger with electric motor
CN102312723A (en) Turbocharger
CN218649018U (en) Electronic assembly for use in a vehicle
JPH0882220A (en) Turbo charger
EP3299601A1 (en) Outboard motor unit and marine vessel

Legal Events

Date Code Title Description
AS Assignment

Owner name: ADVANCED PROPULSION TECHNOLOGIES, INC., CALIFORNIA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:PRUSINSKI, THOMAS M.;HOFBAUER, PETER;SCHMIDT, JASON Z.;REEL/FRAME:022299/0840;SIGNING DATES FROM 20060407 TO 20060630

FEPP Fee payment procedure

Free format text: PAT HOLDER NO LONGER CLAIMS SMALL ENTITY STATUS, ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: STOL); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

SULP Surcharge for late payment
REMI Maintenance fee reminder mailed
LAPS Lapse for failure to pay maintenance fees
STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20120422